# N1003Y: 1981 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2011-06-30 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 30, 2011 - Status when cancelled: Sale reported, pending cancellation - Airframe: [Mcdonnell Douglas DC-9-82(MD-82)](https://openairdocs.org/model/mcdonnell-douglas-dc-9-82-md-82) (registry code 3022082) - Engine: [Pratt & Whitney JT8D series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs) - Serial number: 48068 - Year built: 1981 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: June 8, 1995 - Last registry action: December 12, 2006 - Mode S code: A0078C - Location: Xxx, Mexico - Owner type: Individual - The mark today: https://openairdocs.org/aircraft/N1003Y - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=1003Y - Page: https://openairdocs.org/deregistered/N1003Y-2011-06-30 From the FAA registry file of November 5, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Mcdonnell Douglas DC-9-82(MD-82): https://openairdocs.org/model/mcdonnell-douglas-dc-9-82-md-82.md ## Service difficulty reports (30) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ASMF200608013](https://openairdocs.org/sdr/ASMF200608013), Aug 17, 2006: LOCK. MISINSTALLED. AIRCRAFT RETURNED, RT LANDING GEAR RED LIGHT AND (GEAR DOOR OPEN) LIGHT, REMAINED ON. THEREFORE, ABNORMAL PROCEDURE WAS PERFORMED. DURING MAINTENANCE REVIEW, TH - [SDR ASMF200607015](https://openairdocs.org/sdr/ASMF200607015), Jul 22, 2006: RIVET. LOOSE. REPORTED A WATER LEAK IN THE OVERHEAD PANEL NEAR TO THE CABIN CREW DOOR. AIRCRAFT WAS SENT TO THE HANGAR AND INTERIORS AND AIR CONDITIONING DUCTS WERE REMOVED, - [SDR ASMF200604013](https://openairdocs.org/sdr/ASMF200604013), Apr 25, 2006: FAN BLADE. DAMAGED. DURING TRANSIT CHECK, IT WAS DETECTED ONE LEFT ENGINE C1 FAN BLADE DAMAGED BY AN SCREW SANK INTO THE ACOUSTIC PANEL (FOD). THE DAMAGE WAS EVALUATED IAW M/M 72-0 - [SDR ASMF200501201](https://openairdocs.org/sdr/ASMF200501201), Dec 22, 2005: ENGINE. VIBRATION. CAPTAIN REPORTED THAT DURING FLIGHT WITH EPR BETWEEN 1.0 AND 1.2 IN THE LT ENGINE; VIBRATION AMPLITUDE OCCASIONALLY WITH PEAKS FROM 4 TO 0 AND WHEN THE LT ENGIN - [SDR ASMF200512007](https://openairdocs.org/sdr/ASMF200512007), Dec 7, 2005: PIN. BROKEN. DURING PUSH BACK THE NOSE LANDING GEAR TOWING FUSE PIN WAS BROKEN. IT WAS REPLACED IAW MM 32-21-14 AND THE NOSE LANDING GEAR AND GENERAL INSPECTIONS FOR EXCESSI - [SDR ASMF200507018](https://openairdocs.org/sdr/ASMF200507018), Jul 24, 2005: WARNING LIGHT. ILLUMINATED. CAPTAIN REPORTED THAT AFTER TAKE OFF AFT STAIRWAY DOOR LIGHT TURN ON. DURING REVISION LEFT HOOK WAS DETECTED NOT SECURED AT AFT STAIRWAY DOOR. REPORT WAS DEFERR - [SDR ASMF200506019](https://openairdocs.org/sdr/ASMF200506019), Jun 17, 2005: CONTROL CABLE. BROKEN. AFTER LANDING WHILE TAXING, THE STEERING WENT LOOSE. DURING CHECK, THE STEERING CABLE WAS DETECTED BROKEN. AIRCRAFT WAS SENT TO THE HANGAR AND STEERING CABLE WA - [SDR ASMF200506014](https://openairdocs.org/sdr/ASMF200506014), Jun 11, 2005: UNKNOWN. UNKNOWN. CAPTAIN REPORTED BOTH AIR CONDITION PACKS WITH LOW FLOW AND DURING DESCENT IT WAS NECESSARY TO MAINTAIN THRUST. BOTH A/A PILOT AND PNEUMATIC REGULATORS WERE REP - [SDR ASMF200503018](https://openairdocs.org/sdr/ASMF200503018), Mar 24, 2005: CONNECTOR. FAILED. AIRCRAFT WAS RECEIPT AT GDL WITH CAPTAIN REPORT "VHF 1 OUT OF SERVICE", AS A CORRECTIVE ACTION BOTH VHF WERE REPLACED AN TESTED, ALL CORRECT. AIRCRAFT RETURNED - [SDR ASMF200502003](https://openairdocs.org/sdr/ASMF200502003), Feb 6, 2005: VALVE. LEAKING. DURING TRANSIT CHECK WERE DETECTED HYDRAULIC LEAK AT RIGHT MAIN LANDING GEAR IN VALVE LOCKOUT. THE VALVE LOCKOUT WAS REPLACED IAW MM 32-42-06, TESTED CORRECT. C - [SDR ASMF200412011](https://openairdocs.org/sdr/ASMF200412011), Dec 25, 2004: CONNECTOR. FAILED. AIRCRAFT RETURNED TO PLATFORM DUE TO NO FUEL INDICATION IN BOTH CHANNELS. SEM CONNECTORS WERE CHECKED DETECTING ONE CHANNEL LOOSEN, THE FOUR CHANNELS WERE DISCO - [SDR ASMF200410005](https://openairdocs.org/sdr/ASMF200410005), Oct 7, 2004: MODULATOR. LEAKING. DURING LT ENGINE STARTING CAPTAIN REPORTED LT HYDRAULIC SYSTEM LEAKAGE AND PRESSURE DROP TO ZERO. DURING REVISION THE TECHNICAL PERSONNEL DETECTED THAT THE LEAK - [SDR ASMF200408022](https://openairdocs.org/sdr/ASMF200408022), Aug 26, 2004: THERMOCOUPLE. DAMAGED. DURING OVERNIGHT SERVICE WAS DETECTED RT ENGINE WITH HIGH EGT INDICATION. EGT INDICATION WAS CHECKED IAW MM 77-21-00 AND THERMOCOUPLE NR 4 WAS DETECTED WITH DAM - [SDR ASMF200408003](https://openairdocs.org/sdr/ASMF200408003), Aug 3, 2004: CONTROL VALVE. DAMAGED. CAPTAIN REPORTED, DURING CLIMB "LT REVERSE ACCUMULATOR" LIGHT TURNED ON AND LT HYDRAULIC QUANTITY DOWN AT 4 QUARTERS. LT REVERSE VALVE WAS CHECKED AND LEAK ON P - [SDR ASMF200407013](https://openairdocs.org/sdr/ASMF200407013), Jul 9, 2004: ACTUATOR. FAILED. AIRCRAFT RETURNED AFTER TAKEOFF , IT WAS NOT POSSIBLE TO RETRACT THE NOSE LANDING GEAR WITH STRONG NOISE IN SUCH AREA. THREE FULL EXTENSION AND RETRACTION CYCLE - [SDR ASMF200406025](https://openairdocs.org/sdr/ASMF200406025), Jun 22, 2004: LINK. FAILED. AIRCRAFT RETURNED OF FLIGHT, STRONG VIBRATION IN NOSE LANDING GEAR. DURING MAINTENANCE CHECK WAS DETECTED LT NOSE LANDING GEAR DOOR OPENED, DOOR AND ACTUATOR WE - [SDR ASMF200406022](https://openairdocs.org/sdr/ASMF200406022), Jun 21, 2004: COMPUTER. FAILED. DURING TRANSIT CHECK, CAPTAIN REPORTED SPEED FLAG IN BOTH ADI´S AND FLAG IN EPR LIMIT INDICATOR. CADC´S AND DFGC´S RESEAT WERE PERFORMED AND FAIL CONTINUED. DIF - [SDR ASMF200406001](https://openairdocs.org/sdr/ASMF200406001), Jun 1, 2004: STRINGER. LEAKING. DURING TRANSIT CHECK, A WATER LEAK WAS DETECTED ON UPPER CREW CABIN. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE AIRCRAFT WAS PRESSURIZED AND L - [SDR ASMF200405011](https://openairdocs.org/sdr/ASMF200405011), May 7, 2004: ENGINE. MALFUNCTIONED. AIRCRAFT SUSPENDED TAKE OFF AND RETURNED TO PLATFORM, LOW POWER ON RT ENGINE. INLET AND OUTLET OF RT ENGINE WERE CHECKED, ALL CORRECT. FUEL CONTROL UNIT WAS REP - [SDR ASMF20040403](https://openairdocs.org/sdr/ASMF20040403), Apr 5, 2004: TRANSCEIVER. FAILED. AIRCRAFT ARRIVED WITH FOLLOWING REPORTS: RADAR ANTENNA TURNED TO RIGHT. RADAR CONNECTOR WAS RESEATED AND CLEANED IAW MM 34-41-01. L ICE PROTECT TEMP HIGH LIGHT - [SDR MEX2004052](https://openairdocs.org/sdr/MEX2004052), Feb 11, 2004: WARNING SYSTEM. FAILED. FLT 278 - MEX-CJS - AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURNIG PUSH-BACK APU SHUTOFF AND APU FIRE, OVERSPEED, AND TAKEOFF ALARMS WERE ACTIVATED. A - [SDR MEX2004053](https://openairdocs.org/sdr/MEX2004053), Feb 11, 2004: RECEPTACLE. DAMAGED. FLT 278 - MEX-CJS - AIRCRAFT RETURNED DUE TO NOSE LANDING GEAR RED LIGHT TURNED ON. DURING CHECK IT WAS DETECTED A WIRE BROKEN IN THE NOSE LANDING GEAR DOWN SEN - [SDR MEX2003459](https://openairdocs.org/sdr/MEX2003459), Oct 3, 2003: WHEEL. STUCK. AIRCRAFT RETURN TO PLATFORM DUE TO TAXING VIBRATION WS FELT ON THE BRAKES AND THE AIRCRAFT STOPS BY ITSELF. DURING REVISION WAS DETECTED THE BRAKE NUMBER THREE - [SDR MEX2003198](https://openairdocs.org/sdr/MEX2003198), Jun 1, 2003: INDICATOR. FAILED. AIRCRAFT SUSPENDS TAKEOFF DUE TO AIRSPEED INDICATIONS SHOWED A 40 KNOTS DIFFERENCE AND SPEED FLAG APPEARED. THE MACH AND AIRSPEED INDICATOR NR 2 WERE REPLACED I - [SDR MEX2003064](https://openairdocs.org/sdr/MEX2003064), Mar 9, 2003: ENGINE. LACK OF LUBE. FLT 940 - MEX-MTY, AIRCRAFT RETURNED TO PLATFORM, DURING TAXIING THE LOW QUANTITY OIL LIGHT OF ENGINE NR 2 TURNED ON. THE OIL LEVEL WAS VERIFIED BEING NECESSARY - [SDR MEX2003009](https://openairdocs.org/sdr/MEX2003009), Jan 22, 2003: PUMP. FAILED. FLT 258 - MEX-CJS - AIRCRAFT RETURNED TO GATE DUE TO LEFT ENGINE HYDRAULIC PUMP OUT OF SERVICE WITH CERO PRESSURE INDICATION. LEFT ENGINE HYDRAULIC PUMP WAS REP - [SDR MEX2002384](https://openairdocs.org/sdr/MEX2002384), Dec 28, 2002: WARNING LIGHT. ILLUMINATED. AIRCRAFT RETURN TO FLIGHT DUE TO ACCESSORY COMPARTMENT DOOR LIGHT TURNED ON. COMPARTMENT DOOR WAS CHECKED DETECTING TWO SECURES UNSAFE, REINSTALLED. DURING OVER - [SDR MEX2002298](https://openairdocs.org/sdr/MEX2002298), Sep 13, 2002: COVER. DETACHED. FLT 509 - MEX-VSA - AIRCRAFT RETURNED TO PLATFORM AS CONSEQUENCE OF THAT THE SLIDE RAFT COVER OF THE REAR SERVICE DOOR WAS DETACHED. THE TECHNICIANS DETECTED TH - [SDR MEX2002038](https://openairdocs.org/sdr/MEX2002038), Feb 13, 2002: RELAY. FAILED. FLT 119 - TIJ-GDL - PILOT REPORTED THAT L HYD PRESS LOW LIGHT DOES NOT TURN ON. LOW PRESSURE SWITCH WAS CHECKED AN SEVERAL CYCLES WERE PERFORMED WITH THE CONTRO - [SDR MEX2002135](https://openairdocs.org/sdr/MEX2002135), Feb 5, 2002: HYDRAULIC LINE. LEAKING. FLT 136 - MEX-AGS - FIFTEEN MINUTES BEFORE TAKEOFF, WHEN THE CAPTAIN TRIED TO PRESSURE THE HYDRAULIC SYSTEM A HYDRAULIC LEAK WAS DETECTED AT THE TAIL CONE AREA. ## Other aircraft with N1003Y - [Cancelled 2020-12-04](https://openairdocs.org/deregistered/N1003Y-2020-12-04): Thrush S2R-T34, S/N T34-492, built 2019. Expired dealer. Owner: [Thrush Aircraft Inc](https://openairdocs.org/faa-owner/THRUSH%20AIRCRAFT%20INC), [Albany, GA](https://openairdocs.org/faa-place/GA/Albany) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.